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A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool /

Bibliographic Details
Main Authors:	Csank, Jeffrey T. (Author), Stueber, Thomas J. (Author)
Corporate Author:	Joint Propulsion Conference and Exhibit
Format:	Government Document Conference Proceeding eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
Series:	NASA technical memorandum ; 2012-217714.
Subjects:	Computerized simulation. Propulsion system configurations. Wind tunnel tests. Fuel systems. Propulsion system performance. Turbine engines. Engine inlets.
Online Access:	https://purl.fdlp.gov/GPO/gpo33018

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